发明名称 SPACECRAFT POSITION ESTIMATING SYSTEM AND METHOD
摘要 FIELD: radio engineering, communication.SUBSTANCE: system includes receiving stations (4) for receiving signals transmitted from the spacecraft (6) and a processing station (2) for receiving data from the receiving stations (4), where each receiving station (4) records, during a recording window (8), signals transmitted from the spacecraft (6) and transmits, to the processing station (2), data representing the recorded signals. The recording windows (8) associated with each of the receiving stations (4) are offset and/or have different size with respect to each other. The processing station (2) correlates the recorded signals to estimate the distance difference between the spacecraft (6) and each of a plurality of receiving stations and to estimate the spacecraft (6) position.EFFECT: avoiding the need to send a reference signal pattern, emission by the spacecraft of any trigger sequence and the need to adapt the spacecraft, and improved estimation of the position of the spacecraft.22 cl, 10 dwg, 1 tbl
申请公布号 RU2508558(C2) 申请公布日期 2014.02.27
申请号 RU20110106746 申请日期 2009.07.23
申请人 SES ASTRA S.A. 发明人 TILL' MARK;ARL' GI;GROSS MARKUS;VAUTERS JOS;KRIE ZHORZH
分类号 G01S5/06;G01S19/00 主分类号 G01S5/06
代理机构 代理人
主权项
地址